Crash of a Cessna 208B Grand Caravan near Postville: 1 killed

Date & Time: Feb 8, 1991 at 0812 LT
Type of aircraft:
Operator:
Registration:
C-FPEZ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Nain - Goose Bay
MSN:
208B-0120
YOM:
1988
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While on a cargo flight from Nain to Goose Bay, the pilot reported problems to ATC and was cleared to descend from 7,500 to 3,500 feet. Shortly later, the aircraft entered an uncontrolled descent and stuck the ground in a 55° nose-down attitude some 51 southwest of Postville. The pilot, sole on board was killed. At the time of the accident, weather conditions were considered as good without any icing conditions or atmospheric turbulences.
Probable cause:
The exact cause of the accident could not be determined.

Crash of a Cessna 441 Conquest in Greenland: 8 killed

Date & Time: Sep 12, 1990 at 1745 LT
Type of aircraft:
Operator:
Registration:
OY-CGM
Flight Phase:
Survivors:
No
Schedule:
Söndreströmfjord - Goose Bay
MSN:
441-0229
YOM:
1982
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The twin engine aircraft departed Sondreströmfjord on a charter flight to Goose Bay, carrying six sailors and two pilots. Seventeen minutes after takeoff, while cruising at FL220, the aircraft entered an uncontrolled descent and the crew did not send any distress call. At an altitude of 7,000 feet, the aircraft disintegrated and debris scattered on a wide area. The wreckage was found about 148 southwest of Sondreströmfjord and all eight occupants were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty. However, the following findings were reported:
- There was no evidence from the post-mortem examination which suggests a contributory factor in this accident.
- There was no radio transmission from the crew indicating that they were concerned of any problem.
- There was no evidence of fire, engine failure, explosion, structural or mechanical defect prior to the in-flight break-up.
- The evaluation of the ATC tape indicates that an impairment of the crew was present, consistent with, but not confirmatory of hypoxia.

Crash of a Dassault Falcon 20D off Keflavik

Date & Time: Oct 11, 1987 at 1852 LT
Type of aircraft:
Operator:
Registration:
EC-EFI
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
West Palm Beach – Bedford – Goose Bay – Keflavik
MSN:
189
YOM:
1969
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Recently purchased by the Spanish operator Drenair, the aircraft departed West Palm Beach, Florida, on a delivery flight to Spain, carrying four passengers and two pilots. After a fuel stop in Bedford, Massachusetts, and Goose Bay, Newfoundland, the aircraft continued to Keflavik, Iceland. While approaching Keflavik, the crew declared an emergency due to fuel exhaustion, informed ATC about his position and ditched the aircraft approximately 70 km southwest of Keflavik. All six occupants were quickly rescued by the crew of a helicopter while the aircraft sank and was lost.
Probable cause:
It is believed that the crew encountered strong and unexpected headwinds, causing a higher fuel consumption than calculated. Due to fuel exhaustion, the crew was forced to ditch the aircraft. It is unclear if both engines failed or not prior to ditching.

Crash of a De Havilland DHC-3 Otter near Goose Bay: 4 killed

Date & Time: Mar 24, 1986 at 0955 LT
Type of aircraft:
Registration:
C-FAGM
Flight Phase:
Survivors:
Yes
Schedule:
Snegamook Lake - Goose Bay
MSN:
400
YOM:
1961
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
4
Aircraft flight hours:
13258
Circumstances:
A wheel/ski-equipped DHC-3 Otter aircraft was on the return leg of a charter flight to Snegamook Lake to retrieve a hunting party of four, along with their hunting gear and bounty of several hundred ptarmigan. It departed Snegamook Lake at 09:15. After takeoff, the engine began to run rough but improved somewhat when the power was reduced for cruising. As the aircraft was approaching Nipishish Lake, the pilot reported to company dispatch that the engine was again running rough, but he was able to maintain altitude, and he would follow the Crooked River toward Goose Bay in case a precautionary landing became necessary. Three minutes later, C-FAGM called dispatch again, advising them that he was intending to land on a large area on the Crooked River. He also indicated that there was an odour of smoke in the aircraft. The aircraft was in a nose-down, left- bank attitude, with the flaps fully extended and the skis retracted when it struck the frozen surface of the river. The Otter bounced clear of the surface, turned left came to rest in an upright position.
Probable cause:
It was determined that a fatigue-initiated crack in the number nine cylinder head caused the engine to run rough and lose power. While the pilot was manoeuvring for the precautionary landing in whiteout conditions, the aircraft crashed. At impact, the fuel cells ruptured, and a fire erupted which destroyed the aircraft.

Crash of a De Havilland DHC-6 Twin Otter 100 in Goose Bay: 4 killed

Date & Time: Oct 11, 1984 at 1737 LT
Operator:
Registration:
C-FAUS
Flight Type:
Survivors:
No
Schedule:
Saint Anthony - Goose Bay
MSN:
34
YOM:
1967
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Aircraft flight hours:
17585
Circumstances:
The Twin Otter departed Goose Bay on a medical evacuation flight to St. Anthony. The flight was uneventful and landed in St. Anthony at 15:24. At 16:02, the aircraft departed St. Anthony on a VFR flight back to Goose Bay. On board were the two pilots and the doctor and nurse. Approaching the Goose Bay Airport, weather became marginal, but the crew continued visual flight. The crew likely encountered near zero forward visibility in snow showers and fog; it is probable that they were able to maintain vertical contact with the ground and were confident they could continue flight with visual reference to the ground. The crew may not have been able to see terrain ahead and therefore may not have been able to determine if the aircraft would clear the hills, particularly, when steep hills were encountered. The plane struck a rock outcropping 100 feet below the summit of a 2,050-foot mountain. After bouncing twice, the Twin Otter had come to rest in a small, wooded gully, approximately 350 feet from the initial point of impact.
Probable cause:
It was determined that the flight was attempted in mountainous terrain in marginal weather conditions. The aircraft was flown at an altitude which did not provide terrain clearance, and the aircraft struck a mountain for undetermined reasons.

Crash of a Cessna 402A in the Atlantic Ocean: 2 killed

Date & Time: Jan 19, 1981
Type of aircraft:
Operator:
Registration:
C-GDTW
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Goose Bay - Keflavik
MSN:
402A-0037
YOM:
1979
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While on a ferry flight from Goose Bay to Keflavik, the twin engine airplane crashed in unknown circumstances in the North Atlantic Ocean. Both occupants were killed.

Crash of a Aviation Traders ATL-98 Carvair in Twin Falls

Date & Time: Sep 28, 1968
Operator:
Registration:
CF-EPX
Survivors:
Yes
Schedule:
Goose Bay – Twin Falls
MSN:
6/7480
YOM:
1944
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
33
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, who had limited experience on Carvair aircraft, possibly wanted to touch down as early as possible on the short runway. The main wheels however struck the top of an embankment about 8 feet from the runway threshold. The pilot overshoot and had to feather the no. 2 prop immediately, because the engine was not developing power. The aircraft circled for a while and then touched down on its nosegear. The plane settled on the left wing and swung off the runway.
Probable cause:
The pilot's distraction with the landing hazard led him to attempt a touchdown dangerously close to the runway threshold. The pilot was assigned to perform a landing on a marginal landing area.

Crash of a Dassault Falcon 20C in Goose Bay

Date & Time: Oct 1, 1967
Type of aircraft:
Registration:
HB-VAP
Survivors:
Yes
Schedule:
Geneva – Keflavik – Goose Bay
MSN:
37
YOM:
1966
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was completing a transatlantic flight from Geneva to Goose Bay with an intermediate stop in Keflavik. On final approach to Goose Bay Airport, both engines failed simultaneously. The crew realized he could not reach the airport so the captain decided to attempt an emergency landing. The airplane belly landed, slid for several yards and came to rest 11 km short of runway. All seven occupants were rescued while the aircraft was damaged beyond repair.
Probable cause:
Double engine failure on approach caused by a fuel exhaustion.

Crash of a Douglas C-133A-30-DL Cargomaster in Goose Bay: 7 killed

Date & Time: Nov 7, 1964 at 1649 LT
Type of aircraft:
Operator:
Registration:
56-2014
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Dover – Goose Bay – Sondreströmfjord - Thule
MSN:
45251
YOM:
1956
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The ill-fated aircraft that crashed was a Douglas C-133A Cargomaster s/n 56-2014 from Military Air Transport Service’s 1st Air Transport Squadron, based at Dover Air Force Base in Delaware. It arrived at Goose Bay 01:55 hours local time. After a 15-hour crew rest, they proceeded to depart enroute to Thule Air Base, Greenland with a stop enroute at Sondrestrom Air Base, also in Greenland. They were loaded with meat and other provisions. The first departure attempt was delayed due to a technical issue. The aircraft sat for a period of time without being de-iced before making a second try. At between 120 and 150 feet, the aircraft’s starboard (right) wing suddenly dropped 20 to 30 degrees. The aircraft commander managed to momentarily regain a level attitude. The aircraft then rolled to the left. The port wing dropped even more quickly and was almost vertical. The aircraft commander was unable to do anything. At 16:49 hrs local time, the Cargomaster struck the ground in a left wing down, nose high attitude.
Crew:
1st Lieutenant Guy L. Vassalotti, pilot,
Cpt Charles L. Jenkins, copilot,
Maj Frank X. Hearty, copilot,
1st Lt Douglas H. Brookfield, navigator,
T/Sgt John. A. Kitchens, flight engineer,
T/Sgt Norman H. Baron, flight engineer,
A1c Shelton Toler, loadmaster.
Probable cause:
After an intensive investigation, the accident investigation board determined the primary cause was a power stall. The most probable reason was structural icing of the wing and /or vortex generators that had accumulated ice over the 15-hour layover.

Crash of a Douglas DC-4 near Issoudun: 79 killed

Date & Time: Aug 11, 1957 at 1415 LT
Type of aircraft:
Operator:
Registration:
CF-MCF
Flight Phase:
Survivors:
No
Schedule:
London – Keflavik – Goose Bay – Toronto
MSN:
18374
YOM:
1944
Location:
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
73
Pax fatalities:
Other fatalities:
Total fatalities:
79
Captain / Total flying hours:
13500
Captain / Total hours on type:
1000.00
Circumstances:
CF-MCF departed London, England at 2148 GMT on 10 August on a charter flight to Toronto, Canada, with planned refuelling stops at Keflavik, Iceland and Goose Bay, Labrador. It carried a crew of 6 and 73 passengers (including 2 infants) The aircraft departed from Keflavik at 0512 GMT on 11 August, after a stop of 1 hour 6 minutes during which it was refuelled to capacity. At 1320 GMT it advised that it would overfly Goose Bay and proceed to Montreal. It arrived over Goose Bay at 1403, nineteen minutes ahead of its ETA, over Seven Islands at 1558 GMT and over Quebec Radio Range at 1807 hours Quebec Radio Range Station relayed a message to the aircraft at 1810 requesting it to contact Montreal Range approaching Rougemont for clearance - this was the last contact with the aircraft. While cruising at an altitude of 6,000 feet, the aircraft went through a thunderstorm area, went out of control and entered a spin. In a 70° nose-down attitude, the airplane struck the ground at a speed of 200 knots and disintegrated in a field located 7 km west of Issoudun. All 79 occupants have been killed.
Probable cause:
The accident was attributed to severe turbulence encountered whilst flying in a cumulonimbus cloud, resulting in a chain of events quickly leading up to a complete loss of control and causing the aircraft to dive to the ground m a near vertical nose-down attitude.
Final Report: